CN108263632A - Unmanned plane transports and launch vehicle - Google Patents
Unmanned plane transports and launch vehicle Download PDFInfo
- Publication number
- CN108263632A CN108263632A CN201810203564.3A CN201810203564A CN108263632A CN 108263632 A CN108263632 A CN 108263632A CN 201810203564 A CN201810203564 A CN 201810203564A CN 108263632 A CN108263632 A CN 108263632A
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- unmanned plane
- cabin
- fixed
- wing
- launch
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- 230000032258 transport Effects 0.000 title description 9
- 230000007246 mechanism Effects 0.000 claims abstract description 8
- 230000007306 turnover Effects 0.000 claims description 10
- 238000005096 rolling process Methods 0.000 claims description 9
- 230000008878 coupling Effects 0.000 claims description 3
- 238000010168 coupling process Methods 0.000 claims description 3
- 238000005859 coupling reaction Methods 0.000 claims description 3
- 230000007704 transition Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P1/00—Vehicles predominantly for transporting loads and modified to facilitate loading, consolidating the load, or unloading
- B60P1/52—Vehicles predominantly for transporting loads and modified to facilitate loading, consolidating the load, or unloading using rollers in the load-transporting element
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
- B64F1/222—Ground or aircraft-carrier-deck installations for handling aircraft for storing aircraft, e.g. in hangars
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Conveying And Assembling Of Building Elements In Situ (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses a kind of transport of unmanned plane and launch vehicles, including automobile chassis, truck-mounted crane, several jack supporting mechanisms, combine shelter and unmanned plane launch device, it combines shelter and includes attachment cabin and wing storage cabin, wing storage bilge portion is fixed on automobile chassis, attachment cabin is vertically fixed on one end at the top of wing storage cabin, unmanned aerial vehicle body storage box is fixed on the middle part in wing storage cabin, fuselage is fixed on by binding strap on unmanned aerial vehicle body storage box bottom plate, unmanned plane launch device is fixed on the other end at the top of wing storage cabin.The present invention is compact-sized, rationally distributed, saves memory space.The unmanned plane launch device of the present invention selects best launch angle convenient for unmanned plane, improves the safety that unmanned plane takes off, and has saved transition and has taken off cost, has improved the service efficiency of unmanned plane.
Description
Technical field
The present invention relates to a kind of storage means of transport of unmanned plane, more particularly to a kind of unmanned plane transport shelter further relates to
A kind of vehicle transmitting platform of unmanned plane belongs to
In special vehicle technical field.
Background technology
UAV（Hereinafter referred to as unmanned plane）It is widely used in aerial reconnaissance, monitoring, communication, antisubmarine and electronic interferences
Deng.In actual use, unmanned plane is needed continually to store and be transported with transition, and the span of unmanned plane wing is longer, more than highway
The width limitation of transport, it is necessary to could carry out highway transportation after removing the wing of unmanned plane.How decouple after unmanned plane is realized
Wing and fuselage store entrucking respectively, with safe and reliable when ensureing its transport；It can conveniently and efficiently be assembled again during use, and energy
The launch on haulage vehicle of fast reserve ground is a great problem of unmanned plane application.
Invention content
The purpose of the present invention is to provide a kind of transports of unmanned plane and launch vehicle, the vehicle can realize the machine of unmanned plane
The wing and fuselage store entrucking respectively, and unmanned plane is assembled into after transporting to guard station, and the side of unmanned plane is quickly adjusted on transport vehicle
By its launch behind position.
The present invention is achieved by the following technical programs：
A kind of unmanned plane transport and launch vehicle, including automobile chassis, truck-mounted crane, several jack supporting mechanisms, combination side
Cabin and unmanned plane launch device, truck-mounted crane are located on rear side of driver's cabin, are fixed on automobile chassis；Jack supporting mechanism point
It is not arranged on both ends lower part of the automobile chassis per side；It combines shelter and includes attachment cabin and wing storage cabin, wing storage cabin
Bottom is fixed on automobile chassis, and attachment cabin is adjacent with truck-mounted crane, is vertically fixed on one end at the top of wing storage cabin；Nobody
Machine fuselage storage box is fixed on the middle part in wing storage cabin, and fuselage is fixed on unmanned aerial vehicle body storage box bottom plate by binding strap
On；Unmanned plane launch device is fixed on the other end at the top of wing storage cabin；Rain cover is covered in combination shelter and nothing
On man-machine fuselage storage box.
The purpose of the present invention can also further be realized by following technical measures.
Further, the wing storage Ceiling both ends are equipped with a pair of of rolling guide, pull mesa base both ends point
It is not supported on corresponding rolling guide；The inclined surface of a pair of of wing overlaps up and down, is fixed on pull platform by binding strap；
Downside is supported on two and is disbursed from the cost and expenses on support roller in the middle part of pull platform, and described two are disbursed from the cost and expenses support roller parallel support in wing storage Ceiling
On；Both sides are respectively equipped with several tilt-up doors side by side at the top of wing storage cabin.A pair of locking pins is distinguished by locking pin support base
It is fixed on the outside of corresponding rolling guide, pull platform both sides are respectively equipped with pull platform and pull out the locking with storage in place in place
Hole, when pull platform is pulled out in place with storing in place, locking pin head part, which injects, locks pull platform in corresponding lock hole.
Further, the headlamp out of my cabin that can be lodged is equipped at the top of attachment cabin.
Further, unmanned plane launch device includes turntable and emits oblique frame, and the turntable bottom is fixed on wing
It stores on the other end at the top of cabin, emits oblique frame and include unmanned plane supporting rack and bottom plate, the unmanned plane supporting rack bottom both ends
It is connect with bottom plate by hinged seat and hinge bar, is connect at the top of baseplate underside and turntable respectively.Turntable includes disk shell and position
In direct current generator, worm screw, worm gear and vertical support axis in disk shell, direct current generator bottom is fixed on turntable by support base
On housing bottom, worm screw one end is connect with direct current arbor by shaft coupling, and the worm screw other end is supported on bearing block, bearing block
It is fixed on disk shell bottom；Worm and wheel engages, and is fixedly connected in the middle part of worm gear and vertical support axis, vertical support axis two
End is supported on by vertical support axle bearing in the upper and lower sides of disk shell respectively, and vertical support axis top is stretched out on disk shell
It is fixedly connected behind side with the bottom plate center of unmanned plane supporting rack.
Further, wind one end is injected in disk shell, with the end plug connection of the worm screw other end.
The present invention is compact-sized, rationally distributed, and attachment cabin, unmanned aerial vehicle body storage box and wing storage cabin overlap put up and down
It puts, saves memory space.On the unmanned plane launch device of the present invention is fixed at the top of wing storage cabin, occupied space
It is small.Pass through Worm and Worm Gear Driving in the turntable of unmanned plane launch device so that the oblique frame of transmitting on turntable top can rotate
To required orientation angles, best launch angle is selected convenient for unmanned plane, improves the safety of unmanned plane launch,
It has saved transition to take off cost, has improved the service efficiency of unmanned plane.
The above-mentioned advantage and feature of the present invention, will carry out diagram reconciliation by the non-limitative illustration of preferred embodiment below
It releases, these embodiments only provide as an example with reference to attached drawing.
Description of the drawings
Fig. 1 is the structure diagram of the present invention；
Fig. 2 is the right view of Fig. 1；
Fig. 3 is the structure diagram in wing storage cabin；
Fig. 4 is I enlarged drawing of Fig. 3；
Fig. 5 is the structure diagram of unmanned plane launch device；
Fig. 6 is the A-A cutaway view Amplified images of Fig. 5；
Fig. 7 is the B-B cutaway view Amplified images of Fig. 6.
Specific embodiment
The invention will be further described with reference to the accompanying drawings and examples.
As shown in FIG. 1 to 3, the present embodiment includes automobile chassis 10,1,4 jack supporting mechanism 2 of truck-mounted crane, combination
Shelter 3 and unmanned plane launch device 4, truck-mounted crane 1 are located at 20 rear side of driver's cabin, are fixed on automobile chassis 10, truck-mounted crane 1
It using automatically controlling, folds close at 10 forepart of automobile chassis when not in use, be mainly used for each nacelle, group in lifting combination shelter 3
Unmanned plane 30 after dress and disassemble fuselage 301, wing 302 of state etc..4 jack supporting mechanisms 2 are separately positioned on automobile
On both ends lower part of the chassis 10 per side.4 jack supporting mechanisms 2 of the present embodiment use hydraulic cylinder, are stayed in the present invention
When turner is made, the plunger of 4 hydraulic cylinders drops to ground and four automobile tires 101 is caused to be detached from ground, and pass through vehicle-mounted meter
Calculation machine accurately controls the adjustable height of 4 hydraulic cylinder plungers, thus to the automatic accurate leveling of the present invention, and make its parking steady
It is fixed, it just can ensure that the safety of 30 launch of fuselage 301, the handling of wing 302 and unmanned plane.
It combines shelter 3 and includes attachment cabin 31 and wing storage cabin 32, wing storage 32 bottom of cabin is fixed on automobile chassis 10
On, the attachment cabin 31 being vertically fixed in wing storage 32 top left of cabin is adjacent with truck-mounted crane 1.Unmanned aerial vehicle body storage box 33
It is fixed on the middle part in wing storage cabin 32, fuselage 301 is fixed on unmanned aerial vehicle body storage box bottom plate 331 by binding strap 303
On.Unmanned plane launch device 4 is fixed on the right end at 32 top of wing storage cabin.Rain cover 5 be covered in combination shelter 3,
On unmanned aerial vehicle body storage box 33 and unmanned plane launch device 4.31 top of attachment cabin is equipped with the headlamp out of my cabin that can be lodged
311, provide scene illumination during unmanned plane 30 night launch.
As shown in Fig. 2, 6 inside of turnover panel is stored 32 top both sides of cabin with wing respectively by several hinges 61 and is hinged, nobody
Before machine 30 emits, turnover panel 5 is overturn to horizontality, and 6 downside of turnover panel is supported by hound 62, and 6 outside of turnover panel is equipped with foldable
The guardrail 7 of overturning, such structure stands convenient for personnel and stores operation on the both sides in cabin 32 in wing, and provides reliable peace
All risk insurance hinders, and turnover panel 6 increases the area at 32 top of wing storage cabin, increases personnel operating space.
As shown in Figure 3 and Figure 4,321 both ends of wing storage Ceiling are equipped with a pair of of rolling guide 322, pull platform 323
Bottom both ends are respectively supported on corresponding rolling guide 322.The inclined surface of a pair of of wing 302 overlaps up and down, passes through binding strap
303 are fixed on pull platform 323.323 middle part downside of pull platform is supported on two and is disbursed from the cost and expenses on support roller 324, two row back-up rollers
Sub 324 parallel supports are on wing storage Ceiling 321.As shown in Figure 1, wing storage 32 both sides of cabin are respectively equipped with 7 side by side
A tilt-up door 325 opens tilt-up door 325, you can pulls out pull platform 323, takes out or place a pair of of wing 302.A pair of locking
Pin 326 is separately fixed at corresponding 323 outside of rolling guide by locking pin support base 327, and 323 both sides of pull platform are set respectively
There is pull platform 323 to pull out the lock hole 328 with storage in place in place, when pull platform 323 is pulled out in place with storing in place, lock
Locking pull platform 323 in corresponding lock hole 328 is injected on 326 head of rationed marketing.
As shown in figure 5, unmanned plane launch device 4 includes turntable 41 and emits oblique frame 42,41 bottom of turntable is fixed on
On the right end at 32 top of wing storage cabin, emit oblique frame 42 and include unmanned plane supporting rack 421 and bottom plate 422, unmanned plane supporting rack
421 use the rectangular frame of steel pipe welding, set several cross bars in rectangular frame intermediate parallel so that 421 weight of unmanned plane supporting rack
Amount is relatively light and with just higher intensity.421 bottom both ends of unmanned plane supporting rack pass through hinged seat 423 and hinge bar 424 respectively
It is connect with bottom plate 422 so that emit the 30 launch angle of unmanned plane that oblique frame 42 reaches required, convenient for unmanned plane 30 using fire
Arrow launch assist takes off.
As shown in fig. 6, turntable 41 includes disk shell 411 and direct current generator 412 in disk shell 411, worm screw
413rd, worm gear 414 and vertical support axis 415,412 bottom of direct current generator are fixed on 411 bottom of disk shell by support base 416
On, 413 left end of worm screw is connect with direct current arbor by shaft coupling 417, and 413 right end of worm screw is supported on bearing block 418, bearing
Seat 418 is fixed on 411 bottom right end of disk shell.Worm screw 413 engages with worm gear 414, worm gear 413 and vertical support axis 415
Middle part is fixedly connected by flat key, and 415 both ends of vertical support axis are supported on disk shell by vertical support axle bearing 419 respectively
In 411 upper and lower sides, the bottom plate with unmanned plane supporting rack 421 behind 411 upside of disk shell is stretched out on 415 top of vertical support axis
422 are fixedly connected centrally through several trip bolts.
When power is off, 43 one end of wind can be injected in disk shell 411, inserts its right end end with worm screw 413
It connects in succession.Worm screw 413 is driven to rotate when wind 43 shakes, so as to the worm gear being engaged with 414 be driven to rotate, then by vertical
The driving of support shaft 415 emits oblique frame 42 and turns to required orientation angles or return to home position.Due to the engagement of worm and wormwheel
Self-locking so that emit oblique frame 42 and be locked in required orientation angles, issued convenient for boosting of the unmanned plane 30 in rocket
It penetrates and takes off.
In addition to the implementation, the present invention can also have other embodiment, all to use equivalent substitution or equivalent transformation shape
Into technical solution, all fall within the present invention claims protection domain.
Claims (8)
1. a kind of unmanned plane transport and launch vehicle, including automobile chassis, truck-mounted crane and several jack supporting mechanisms, with vehicle
It hangs on rear side of driver's cabin, is fixed on automobile chassis；Jack supporting mechanism is separately positioned on two of automobile chassis per side
It holds on lower part；It is characterized in that, further including combination shelter and unmanned plane launch device, combination shelter includes attachment cabin and machine
The wing stores cabin, and wing storage bilge portion is fixed on automobile chassis, and attachment cabin is adjacent with truck-mounted crane, is vertically fixed on wing storage
On one end at the top of cabin；Unmanned aerial vehicle body storage box is fixed on the middle part in wing storage cabin, and fuselage is fixed on by binding strap
On unmanned aerial vehicle body storage box bottom plate；Unmanned plane launch device is fixed on the other end at the top of wing storage cabin；Rain-proof
Cover is covered on combination shelter, unmanned aerial vehicle body storage box and unmanned plane launch device.
2. unmanned plane transport according to claim 1 and launch vehicle, it is characterised in that：The wing stores Ceiling
Both ends are equipped with a pair of of rolling guide, and pull mesa base both ends are respectively supported on corresponding rolling guide；A pair of of wing
Inclined surface overlaps up and down, is fixed on pull platform by binding strap；Downside is supported on two and is disbursed from the cost and expenses support roller in the middle part of pull platform
On, described two are disbursed from the cost and expenses support roller parallel support on wing storage Ceiling；Both sides are respectively equipped with side by side at the top of wing storage cabin
Several tilt-up doors.
3. unmanned plane transport according to claim 2 and launch vehicle, it is characterised in that：A pair of locking pins passes through locking
Pin support base is separately fixed on the outside of corresponding rolling guide, and pull platform both sides are respectively equipped with pull platform and pull out in place and receive
The lock hole received in place, when pull platform is pulled out in place with storing in place, locking pin head part, which is injected in corresponding lock hole, to be locked
Pull platform.
4. unmanned plane transport according to claim 1 and launch vehicle, it is characterised in that：Pass through several hinges on the inside of turnover panel
Chain is hinged respectively with both sides at the top of wing storage cabin, and before unmanned plane transmitting, turnover panel is overturn to horizontality, and turnover panel downside is by oblique
Strut supports, and the guardrail of folding turnover is housed on the outside of turnover panel.
5. unmanned plane transport according to claim 1 and launch vehicle, it is characterised in that：It is equipped with to fall at the top of attachment cabin
The headlamp out of my cabin of volt.
6. unmanned plane transport according to claim 1 and launch vehicle, it is characterised in that：Unmanned plane launch device
Including turntable and emit oblique frame, the turntable bottom is fixed on the other end at the top of wing storage cabin, is emitted oblique frame and is included nothing
Man-machine supporting rack and bottom plate, the unmanned plane supporting rack bottom both ends are connect respectively by hinged seat and hinge bar with bottom plate, bottom
With being connect at the top of turntable on the downside of plate.
7. unmanned plane transport according to claim 6 and launch vehicle, it is characterised in that：Turntable include disk shell and
Direct current generator, worm screw, worm gear and vertical support axis in disk shell, direct current generator bottom is fixed on by support base to be turned
On disk housing bottom, worm screw one end is connect with direct current arbor by shaft coupling, and the worm screw other end is supported on bearing block, bearing
Seat is fixed on disk shell bottom；Worm and wheel engages, and is fixedly connected in the middle part of worm gear and vertical support axis, vertical support axis
Both ends are supported on by vertical support axle bearing in the upper and lower sides of disk shell respectively, and disk shell is stretched out on vertical support axis top
It is fixedly connected behind upside with the bottom plate center of unmanned plane supporting rack.
8. unmanned plane transport according to claim 7 and launch vehicle, it is characterised in that：Turntable is injected in wind one end
In housing, with the end plug connection of the worm screw other end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810203564.3A CN108263632B (en) | 2018-03-13 | 2018-03-13 | Unmanned aerial vehicle transportation and launching galloping |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810203564.3A CN108263632B (en) | 2018-03-13 | 2018-03-13 | Unmanned aerial vehicle transportation and launching galloping |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108263632A true CN108263632A (en) | 2018-07-10 |
| CN108263632B CN108263632B (en) | 2024-03-19 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810203564.3A Active CN108263632B (en) | 2018-03-13 | 2018-03-13 | Unmanned aerial vehicle transportation and launching galloping |
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| Country | Link |
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| CN (1) | CN108263632B (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109319163A (en) * | 2018-11-12 | 2019-02-12 | 北京特种机械研究所 | A kind of integrated car launcher of transmitting transport |
| CN109813183A (en) * | 2019-01-18 | 2019-05-28 | 江苏捷诚车载电子信息工程有限公司 | Multi rack target drone transshipment vehicle and reprinting method |
| CN110281829A (en) * | 2019-08-05 | 2019-09-27 | 王鸣威 | Go straight up to machine operation resupply vehicle |
| CN110562476A (en) * | 2019-10-10 | 2019-12-13 | 苏州江南航天机电工业有限公司 | Vehicle-mounted unmanned aerial vehicle launching device |
| CN111071162A (en) * | 2019-12-10 | 2020-04-28 | 苏州智加科技有限公司 | Sensor mounting and dismounting method and vehicle |
| CN111392057A (en) * | 2019-12-31 | 2020-07-10 | 航天时代飞鸿技术有限公司 | A on-vehicle machinery device of flying that lets for unmanned aerial vehicle |
| CN111731500A (en) * | 2020-06-15 | 2020-10-02 | 西安爱生技术集团公司 | Propeller unmanned aerial vehicle in-chassis launching simulation method |
| CN113859093A (en) * | 2021-10-27 | 2021-12-31 | 北京金朋达航空科技有限公司 | Integrated unmanned aerial vehicle transportation launching device |
| CN114167881A (en) * | 2021-10-27 | 2022-03-11 | 南京航空航天大学 | Aerial unmanned aerial vehicle launching and recovering platform, working method and aerial taking-off and landing platform |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109319163A (en) * | 2018-11-12 | 2019-02-12 | 北京特种机械研究所 | A kind of integrated car launcher of transmitting transport |
| CN109813183B (en) * | 2019-01-18 | 2024-03-19 | 江苏捷诚车载电子信息工程有限公司 | Multi-frame target drone transshipment transport vehicle and transshipment method |
| CN109813183A (en) * | 2019-01-18 | 2019-05-28 | 江苏捷诚车载电子信息工程有限公司 | Multi rack target drone transshipment vehicle and reprinting method |
| CN110281829A (en) * | 2019-08-05 | 2019-09-27 | 王鸣威 | Go straight up to machine operation resupply vehicle |
| CN110562476A (en) * | 2019-10-10 | 2019-12-13 | 苏州江南航天机电工业有限公司 | Vehicle-mounted unmanned aerial vehicle launching device |
| CN111071162A (en) * | 2019-12-10 | 2020-04-28 | 苏州智加科技有限公司 | Sensor mounting and dismounting method and vehicle |
| CN111071162B (en) * | 2019-12-10 | 2021-07-30 | 苏州智加科技有限公司 | Sensor mounting and dismounting method and vehicle |
| CN111392057A (en) * | 2019-12-31 | 2020-07-10 | 航天时代飞鸿技术有限公司 | A on-vehicle machinery device of flying that lets for unmanned aerial vehicle |
| CN111392057B (en) * | 2019-12-31 | 2021-06-08 | 航天时代飞鸿技术有限公司 | A on-vehicle machinery device of flying that lets for unmanned aerial vehicle |
| CN111731500A (en) * | 2020-06-15 | 2020-10-02 | 西安爱生技术集团公司 | Propeller unmanned aerial vehicle in-chassis launching simulation method |
| CN114167881A (en) * | 2021-10-27 | 2022-03-11 | 南京航空航天大学 | Aerial unmanned aerial vehicle launching and recovering platform, working method and aerial taking-off and landing platform |
| CN114167881B (en) * | 2021-10-27 | 2023-09-26 | 南京航空航天大学 | Aerial unmanned aerial vehicle emission recovery platform, working method and aerial landing platform |
| CN113859093A (en) * | 2021-10-27 | 2021-12-31 | 北京金朋达航空科技有限公司 | Integrated unmanned aerial vehicle transportation launching device |
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| CN108263632B (en) | 2024-03-19 |
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